View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 27386U 02009A 23029.21020713 .00000286 00000-0 10770-3 0 9993
2 27386 98.2126 5.0688 0001199 88.5278 282.0933 14.38230792 95988
| Epoch (UTC): | 29 January 2023 05:02:41 |
| Eccentricity: | 0.0001199 |
| inclination: | 98.2126° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 5.0688° |
| argument of perigee: | 88.5278° |
| revolutions per day: | 14.38230792 |
| mean anomaly at epoch: | 282.0933° |
| orbit number at epoch: | 9598 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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